Adaptive Regulation of the Position and Yaw angle of an UAV

In this paper, a feedback linearization concept is used to regulate the altitude and the attitude of a quadrotor or UAV type. This UAV is modeled by a strongly nonlinear system and one use the feedback linearization in order to render the input output behaves as a linear and by pole placement technique, a command is developed in order that the position and the orientation follow a prescribed trajectory. In order to testify the robustness of the developed command, Simulations are carried out using Matlab software.